DC Field | Value | Language |
---|---|---|
dc.contributor.author | Lee, Jin-Ik | ko |
dc.contributor.author | Jeon, In-Soo | ko |
dc.contributor.author | Lee, Chang-Hun | ko |
dc.date.accessioned | 2019-02-20T04:52:29Z | - |
dc.date.available | 2019-02-20T04:52:29Z | - |
dc.date.created | 2019-01-29 | - |
dc.date.created | 2019-01-29 | - |
dc.date.issued | 2014-01 | - |
dc.identifier.citation | IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.50, no.1, pp.775 - 780 | - |
dc.identifier.issn | 0018-9251 | - |
dc.identifier.uri | http://hdl.handle.net/10203/250230 | - |
dc.description.abstract | In this paper, a new homing guidance law is introduced based on the energy cost weighted by a Gaussian function in order to shape the missile's trajectory and distribute the acceleration command during the engagement. This law can improve guidance performance by alleviating sensitivity with respect to initial heading error and by reducing the possibility of command saturation through distributing acceleration demand properly. | - |
dc.language | English | - |
dc.publisher | IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC | - |
dc.title | Command-Shaping Guidance Law Based on a Gaussian Weighting Function | - |
dc.type | Article | - |
dc.identifier.wosid | 000336052700055 | - |
dc.identifier.scopusid | 2-s2.0-84900525217 | - |
dc.type.rims | ART | - |
dc.citation.volume | 50 | - |
dc.citation.issue | 1 | - |
dc.citation.beginningpage | 775 | - |
dc.citation.endingpage | 780 | - |
dc.citation.publicationname | IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | - |
dc.identifier.doi | 10.1109/TAES.2013.120353 | - |
dc.contributor.localauthor | Lee, Chang-Hun | - |
dc.contributor.nonIdAuthor | Lee, Jin-Ik | - |
dc.contributor.nonIdAuthor | Jeon, In-Soo | - |
dc.description.isOpenAccess | N | - |
dc.type.journalArticle | Article | - |
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